View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 24298U 26041.89975054 +.00000000 +00000-0 +81962-4 0 00008
2 24298 70.7565 231.9432 0017372 185.7469 174.3454 14.12407937 07
| Epoch (UTC): | 10 February 2026 21:35:38 |
| Eccentricity: | 0.0017372 |
| inclination: | 70.7565° |
| perigee height: | 839 km |
| apogee height: | 864 km |
| right ascension of ascending node: | 231.9432° |
| argument of perigee: | 185.7469° |
| revolutions per day: | 14.12407937 |
| mean anomaly at epoch: | 174.3454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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